[1] Jung B, Kim Y.Guidance laws for anti-ship missiles using impact angle and impact time[C]// AIAA Guidance, Navigation, and Control Conference and Exhibit. USA: AIAA, 2006: 6432.
[2] Bergmann E.A new concept for aircraft formation-keeping guidance[C]// A1AA Guidance Navigation and Control Conference, San Diego, CA, USA: AIAA, 1996: 29-31.
[3] Ishigaki T, Moriyoshi Y, Watanabe T, et al.Thermal plasma treatment of titanium carbide powders: Part II. In-flight formation of carbon-site vacancies and subsequent nitridation in titanium carbide powders during induction plasma treatment[J]. Journal of Materials Research(S0884-2914), 1996, 11(11): 2811-2824.
[4] Pachter M, D'Azzo J, Dargan J L. Automatic formation flight control[J]. Journal of Guidance, Control, and Dynamics (S0731-5090), 1994, 17(6): 1380-1383.
[5] Corcoran III J J. Automatic formation flight control system (AFFCS)—a system for automatic formation flight control of vehicles not limited to aircraft, helicopters, or space platforms: U.S. Patent 6, 926, 233 [P].2005-8-9.
[6] 苏建敏, 董云峰. 利用人工势函数法的卫星电磁编队控制[J]. 北京航空航天大学学报, 2012(2): 213-217, 238.
(JianMin Su, Yunfeng Dong. Artificial potential function method for satellite electromagnetic formation control[J]. Journal of Beijing University of Aeronautics and Astronautics, 2012(2): 213-217, 238.)
[7] 秦世引, 潘宇雄, 苏善伟. 小型无人机编队飞行的控制律设计与仿真[J]. 智能系统学报, 2009(3): 218-225.
[8] Chen J, Sun D, Yang J, et al.A leader-follower formation control of multiple nonholonomic mobile robots incorporating receding-horizon scheme[J]. The International Journal of Robotics Research (S0278-3649), 2009:1134-1137.
[9] Soorki M N, Talebi H A, Nikravesh S K Y. A robust dynamic leader-follower formation control with active obstacle avoidance[C]// Systems, Man, and Cybernetics (SMC), 2011 IEEE International Conference on. USA: IEEE, 2011: 1932-1937.
[10] Soorki M N, Talebi H A, Nikravesh S K Y. A robust dynamic leader-follower formation control with active obstacle avoidance[C]// Systems, Man, and Cybernetics (SMC), 2011 IEEE International Conference on. USA: IEEE, 2011: 1932-1937.
[11] 马培蓓, 纪军. 多导弹三维编队控制[J]. 航空学报, 2010(8): 1660-1666.
(Peibei M, Jun J.Three- dimensional Multi-missile Formation Control[J]. Acta Aeronautica Et Astronautica Sinica, 2010(8): 1660-1666.)
[12] Wei C, Guo J, Cui N.Research on the missile formation keeping optimal control for cooperative engagement[J]. Journal of Astronautics (S1000-1328), 2010, 31(4): 1043-1044.
[13] 韦常柱, 郭继峰, 崔乃刚. 导弹协同作战编队队形最优保持控制器设计[J]. 宇航学报, 2010, 31(4): 1043-1050.
(Wei C, Guo J, Cui N.Research on the missile formation keeping optimal control for cooperative engagement[J]. Journal of Astronautics, 2010, 31(4): 1043-1050.)
[14] 张磊, 方洋旺, 刁兴华, 等. 多导弹协同攻击编队非线性最优控制器设计[J]. 北京航空航天大学学报, 2014 (3): 401-406.
[15] Chen Q, Ozguner U.A hybrid system model and overlapping decomposition for vehicle flight formation control[C]// Decision and Control, 2003, Proceeding, 42nd IEEE Conference on. USA: IEEE, 2003, 1: 516-521.
[16] Shicai Liu, Dallong Tan, Guangjun Liu.Robust leader-follower formation control of mobile robots based on a second order kinematics model[J]. Acta Automatica Sinica (S0254-4156), 2007, 33(9): 947-955.
[17] 钱杏芳, 林瑞雄, 赵亚男. 导弹飞行力学 [M]. 北京:北京理工大学出版社, 2008: 22-50.
[18] 谷逸宇. 多导弹编队飞行导引律设计[J]. 现代防御技术, 2014, 42(1): 51-55. |
http://www.china-simulation.com
